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Small-sized unmanned aircraft steering engine control device

A technology of unmanned aerial vehicles and control devices, which is applied in the direction of toy aircraft, control starting methods, non-electric variable control, etc., can solve the problems of unseen structurally mature products, etc., and achieve the effect of simple structure, simple programming, and easy realization

Inactive Publication Date: 2009-12-09
JIANGSU WANLI MACHINERY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In view of this, various research institutions have proposed different schemes and devices, but there are no reports of mature products with simple structure, high reliability, simple programming and low price.

Method used

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  • Small-sized unmanned aircraft steering engine control device
  • Small-sized unmanned aircraft steering engine control device
  • Small-sized unmanned aircraft steering engine control device

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0016] A preferred embodiment of the present invention is described as follows in conjunction with accompanying drawing:

[0017] see figure 1 , the small UAV steering gear control device is connected in series between the receiver 5 and the steering gear 6, and the six-way steering gear control signal 13 input from the receiver 5 is input to the CPLD 8, and the CPLD 8 is based on the obtained six-way C steering gear control signal 13 Output the B servo control signal 12 to the signal sampling port of the single chip microcomputer 1. The three-way switching control mode signal 14 input from the receiver 5 is input into the CPLD 8, and the CPLD 8 outputs the mode switching signal 11 to the signal sampling port of the single-chip microcomputer 1 according to the obtained three-way switching control mode signal 14. The single-chip microcomputer 1 communicates with the host computer through the serial port 2, and sends the obtained information of the six-way C steering gear contr...

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PUM

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Abstract

The invention discloses a steering gear control device for a small unmanned aerial vehicle. Its circuit mechanism is that the single-chip microcomputer is connected with the complex programmable logic device CPLD. The single-chip microcomputer is connected to the host computer through the serial peripheral device interface SPI or the universal asynchronous transceiver UART. Access the steering gear. The invention reduces the design complexity of the system and enhances the system's post-modification performance. It is not necessary to modify the hardware of the system, but only to modify the software of the system to achieve the purpose of modifying the system. The invention adopts modular design, has high reliability, simple device debugging and low cost.

Description

technical field [0001] The invention relates to a steering gear control device for a small unmanned aerial vehicle, in particular to a steering gear control device for an ultra-small unmanned helicopter, belonging to the technical field of ultra-small unmanned aerial vehicles. Background technique [0002] The steering gear control system is an important device in the UAV. It is the interface between the flight control computer and the steering gear, and is used to directly operate the steering gear to control the operating state of the aircraft. Due to the small size and light weight of small unmanned aerial vehicles, they are very vulnerable to environmental interference during flight and destroy their autonomous flight. At the same time, small unmanned aerial vehicles often have complex electromagnetic environments, which can easily cause the control system to lose control, and there is often a risk of crashing. In order to avoid flight accidents, it is required that the ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/00B64C13/18A63H27/20
Inventor 冯伟罗均龚振邦高同跃
Owner JIANGSU WANLI MACHINERY